FR2367918A1 - FUEL CONTROL DEVICE FOR GAS TURBINE ENGINE - Google Patents
FUEL CONTROL DEVICE FOR GAS TURBINE ENGINEInfo
- Publication number
- FR2367918A1 FR2367918A1 FR7730515A FR7730515A FR2367918A1 FR 2367918 A1 FR2367918 A1 FR 2367918A1 FR 7730515 A FR7730515 A FR 7730515A FR 7730515 A FR7730515 A FR 7730515A FR 2367918 A1 FR2367918 A1 FR 2367918A1
- Authority
- FR
- France
- Prior art keywords
- piston
- control device
- gas turbine
- turbine engine
- fuel control
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Granted
Links
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
- F02C9/00—Controlling gas-turbine plants; Controlling fuel supply in air- breathing jet-propulsion plants
- F02C9/26—Control of fuel supply
- F02C9/32—Control of fuel supply characterised by throttling of fuel
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Output Control And Ontrol Of Special Type Engine (AREA)
- High-Pressure Fuel Injection Pump Control (AREA)
Abstract
L'invention concerne un dispositif de commande de combustible pour moteur à turbine à gaz. Il comporte un piston doseur 65 manoeuvrable par une servopression qui est commandée par une valve pilote 17, 63. La valve pilote 17, 63 est sensible aux pressions P2, P3 dans le compresseur du moteur et aussi à la position du piston 65. La sensibilité à la position du piston 65 est commandée par un galet 61 mû par un piston 43 et un levier 57. Le piston 43 est lui-même servocommandé par des masselottes 50 agissant sur un manchon 42 qui fournit une autre valve pilote. Application à l'alimentation des turbines à gaz.The invention relates to a fuel control device for a gas turbine engine. It comprises a metering piston 65 which can be operated by a servo-pressure which is controlled by a pilot valve 17, 63. The pilot valve 17, 63 is sensitive to the pressures P2, P3 in the compressor of the engine and also to the position of the piston 65. The sensitivity the position of the piston 65 is controlled by a roller 61 moved by a piston 43 and a lever 57. The piston 43 is itself servo-controlled by weights 50 acting on a sleeve 42 which provides another pilot valve. Application to the supply of gas turbines.
Applications Claiming Priority (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| GB4248576A GB1589966A (en) | 1976-10-13 | 1976-10-13 | Fuel control system for a gas turbine engine |
| GB65577 | 1977-01-07 |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| FR2367918A1 true FR2367918A1 (en) | 1978-05-12 |
| FR2367918B1 FR2367918B1 (en) | 1982-12-03 |
Family
ID=26236107
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| FR7730515A Granted FR2367918A1 (en) | 1976-10-13 | 1977-10-11 | FUEL CONTROL DEVICE FOR GAS TURBINE ENGINE |
Country Status (5)
| Country | Link |
|---|---|
| US (1) | US4187673A (en) |
| JP (1) | JPS5348115A (en) |
| DE (1) | DE2745439A1 (en) |
| FR (1) | FR2367918A1 (en) |
| IT (1) | IT1087764B (en) |
Families Citing this family (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US4473999A (en) * | 1981-11-16 | 1984-10-02 | Lucas Industries Limited | Fuel control system for a gas turbine engine |
| GB8320319D0 (en) * | 1983-07-28 | 1983-09-01 | Lucas Ind Plc | Fuel control system |
| JPH0820325B2 (en) * | 1988-04-04 | 1996-03-04 | 川崎製鉄株式会社 | Slit nozzle jet pressure measuring device |
| US6401446B1 (en) * | 2000-06-23 | 2002-06-11 | Hamilton Sundstrand Corporation | Valve apparatus for providing shutoff and overspeed protection in a gas turbine fuel system |
| US6981359B2 (en) * | 2003-06-16 | 2006-01-03 | Woodward Governor Company | Centrifugal pump fuel system and method for gas turbine engine |
| US9212608B2 (en) | 2013-05-24 | 2015-12-15 | Hamilton Sundstrand Corporation | Low friction fuel metering valve |
| US9849992B2 (en) * | 2016-05-23 | 2017-12-26 | United Technologies Corporation | Inline pressure regulating valve assembly with inlet pressure bias |
| US11378018B2 (en) * | 2020-06-11 | 2022-07-05 | Honeywell International Inc. | Fuel metering system |
Citations (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| FR1161092A (en) * | 1955-08-17 | 1958-08-20 | United Aircraft Corp | Fuel flow control device for engine units of the turbine type |
| FR1197877A (en) * | 1957-01-16 | 1959-12-03 | Gen Electric | Improvements to constant speed regulators for motors |
| US2926494A (en) * | 1956-09-21 | 1960-03-01 | United Aircraft Corp | Fuel control system |
| FR1310696A (en) * | 1961-10-20 | 1962-11-30 | Gen Electric | Fuel control for turbo-reactor |
| FR1352451A (en) * | 1963-03-29 | 1964-02-14 | United Aircraft Corp | Control unit for the fuel supply of turbine engines, especially helicopter engines |
| US3172259A (en) * | 1962-03-02 | 1965-03-09 | Avco Corp | Variable geometry control for gas turbine engines |
| US3187505A (en) * | 1962-08-13 | 1965-06-08 | Woodward Governor Co | Gas turbine fuel regulator |
Family Cites Families (9)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2935136A (en) * | 1954-02-04 | 1960-05-03 | Rotol Ltd | Control systems for power plants |
| US2941601A (en) * | 1954-12-21 | 1960-06-21 | United Aircraft Corp | Fuel control |
| US2857741A (en) * | 1955-08-17 | 1958-10-28 | United Aircraft Corp | Fuel control with feedback |
| GB858773A (en) | 1957-01-16 | 1961-01-18 | Gen Electric | Improvements in gas turbine power plant fuel control systems |
| US2959002A (en) * | 1957-10-23 | 1960-11-08 | United Aircraft Corp | Turbine engine fuel control |
| US3012401A (en) * | 1958-12-31 | 1961-12-12 | United Aircraft Corp | Positive feedback abatement means |
| US3084510A (en) * | 1960-10-26 | 1963-04-09 | Gen Electric | Turbine engine fuel control |
| US3180426A (en) | 1962-03-30 | 1965-04-27 | United Aircraft Corp | Free turbine engine control system |
| US3196613A (en) * | 1963-02-11 | 1965-07-27 | United Aircraft Corp | Fuel control |
-
1977
- 1977-10-07 IT IT28361/77A patent/IT1087764B/en active
- 1977-10-08 DE DE19772745439 patent/DE2745439A1/en not_active Withdrawn
- 1977-10-11 US US05/840,569 patent/US4187673A/en not_active Expired - Lifetime
- 1977-10-11 FR FR7730515A patent/FR2367918A1/en active Granted
- 1977-10-13 JP JP12293277A patent/JPS5348115A/en active Pending
Patent Citations (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| FR1161092A (en) * | 1955-08-17 | 1958-08-20 | United Aircraft Corp | Fuel flow control device for engine units of the turbine type |
| US2926494A (en) * | 1956-09-21 | 1960-03-01 | United Aircraft Corp | Fuel control system |
| FR1197877A (en) * | 1957-01-16 | 1959-12-03 | Gen Electric | Improvements to constant speed regulators for motors |
| FR1310696A (en) * | 1961-10-20 | 1962-11-30 | Gen Electric | Fuel control for turbo-reactor |
| US3172259A (en) * | 1962-03-02 | 1965-03-09 | Avco Corp | Variable geometry control for gas turbine engines |
| US3187505A (en) * | 1962-08-13 | 1965-06-08 | Woodward Governor Co | Gas turbine fuel regulator |
| FR1352451A (en) * | 1963-03-29 | 1964-02-14 | United Aircraft Corp | Control unit for the fuel supply of turbine engines, especially helicopter engines |
Also Published As
| Publication number | Publication date |
|---|---|
| IT1087764B (en) | 1985-06-04 |
| DE2745439A1 (en) | 1978-04-20 |
| FR2367918B1 (en) | 1982-12-03 |
| JPS5348115A (en) | 1978-05-01 |
| US4187673A (en) | 1980-02-12 |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| ST | Notification of lapse |